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== External links ==
== External links ==
[http://www.murphyair.com/ Murphy Aircraft website]
*[http://www.murphyair.com/ Murphy Aircraft website]
[http://www.bush-planes.com/Murphy-Moose.html Bush Planes]
*[http://www.bush-planes.com/Murphy-Moose.html Bush Planes]


==Related content==
==Related content==

Revision as of 20:23, 20 September 2007

A radial-equipped Murphy Moose.

The Murphy Moose is a large high-wing utility monoplane designed to handle nearly any airfield under any conditions. A homebuilt kit aircraft, the Moose can be purchased as a "quick-build" kit which comes partly pre-assembled. Similar in many respects to the de Havilland Canada DHC-2 Beaver, the Moose is cheaper both to buy and to operate.

Builders can choose whether to equip their aircraft with the 269 kW (360 hp) Russian-built Vedeneyev M14P 9-cylinder radial, or the horizontally-opposed 187 kW (250 hp) Lycoming O-540. Both engines allow the Moose to take off in roughly 180 m (600 ft.

Specifications (Moose M-14P)

General characteristics

  • Crew: one pilot
  • Capacity: 3-5 passengers
  • Length: 8.43 m (25 ft 8 in)
  • Wingspan: 11.05 m (36 ft 3 in)
  • Wing area: 16.9 m² (182 ft²)
  • Empty: 816 kg (1,800 lb)
  • Loaded: 1,586 kg (3,500 lb)
  • Powerplant:Vedeneyev M14P supercharged 9-cylinder radial engine, 269 kW (360 hp)

Performance

  • Maximum speed: 281 km/h (175 mph)
  • Range: 1,840 km (1,150 miles)
  • Rate of climb: 458 m/min (1,500 ft/min)
  • Wing loading: 94 kg/m² (19 lb/ft²)
  • Power/Mass: 0.17 kW/kg (0.10 hp/lb)


Related development

Aircraft of comparable role, configuration, and era